ATLAS 5 CENTAUR DEB, 46643
Orbit data source: Space-Track
ATLAS 5 CENTAUR DEB, 46643 is space debris in HEO originally from a launch on Wed, 17 Sep 2014 UTC launched from the Air Force Eastern Test Range (AFETR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
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46643 intel report (Beta)
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Edit Public Description
Expand to show TLE details & history
TLE from 1 week ago
0 ATLAS 5 CENTAUR DEB
1 46643U 14055CT 25191.70621149 -.00000017 00000-0 00000-0 0 9995
2 46643 19.6774 182.0811 4911926 102.4237 314.8351 1.85043912 32150
Epoch: 2025-07-10T16:56Z
TLE epoch observation values (Epoch: 2025-07-10T16:56:56.672Z)
Latitude
-0.00006°
Longitude
-1.06297°
Altitude
17,377.047 km
Speed
4.397 km/s
True Right ascension
12h 08m 10s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
-14.28061°
Longitude
-136.59711°
Altitude
22,674.056 km
Speed
3.636 km/s
Apparent Right ascension
02h 42m 29s
Apparent Declination
-19° 21' 09"
Sunlit
Visualization observer readout
Local Sidereal Time
12:18:05
Azimuth
292.913° NW
Elevation
-52.874°
Doppler factor
1
Orbital elements
Apogee altitude
35,416.115 km
Perigee altitude
7,882.412 km
Semi-major axis
28,027.401 km
Eccentricity
0.49119
Inclination
19.6774°
RAAN
182.0811°
Arg. of periapsis
102.4237°
True anomaly
257.68156°
Mean anomaly
314.8351°
Eccentric anomaly
288.08169°
Mean motion
0.46256 °/min
Orbital period
778.28 mins
BSTAR
0
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Other satellites on launch #55 in the year 2014 (2014-09-17 UTC)
ATLAS 5 CENTAUR DEB Visibility forecast
Observer location: undefined°, undefined°
Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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739 mins | 2025-07-19 10:05:27.798Z | 265.022° W | 2025-07-19 10:45:27.798Z | 200.704° SSW | 31.307° | 2025-07-19 22:24:27.798Z | 98.339° ESE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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